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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1993/6/

Folder.. - Mar 05 2025 11:59:02 PM
Accuracy of rational-function approximations for linear transonic unsteady aerodynamics c20030810 [3].pdfAccuracy of rational-function approximations for linear transonic unsteady aerodynamics c20030810 [3].pdf 372KB Mar 27 2010 11:50:32 PM
Aerodynamic performance effects due to small leading-edge ice (roughness) on wings and tails c20030810 [6].pdfAerodynamic performance effects due to small leading-edge ice (roughness) on wings and tails c20030810 [6].pdf 903KB Mar 27 2010 11:50:32 PM
Aerodynamic shape optimization using sensitivity analysis on third-order Euler equations c20030810 [9].pdfAerodynamic shape optimization using sensitivity analysis on third-order Euler equations c20030810 [9].pdf 1059KB Mar 27 2010 11:50:32 PM
Aerothermodynamic properties of hypersonic flow over radiation-adiabatic surfaces c20030810 [7].pdfAerothermodynamic properties of hypersonic flow over radiation-adiabatic surfaces c20030810 [7].pdf 1025KB Mar 27 2010 11:50:32 PM
Analytical-experimental investigation of free-vibration characteristics of rotating composite I-beams c20030810 [8].pdfAnalytical-experimental investigation of free-vibration characteristics of rotating composite I-beams c20030810 [8].pdf 946KB Mar 27 2010 11:50:32 PM
Author Index c20030810 [2].pdfAuthor Index c20030810 [2].pdf 170KB Mar 27 2010 11:50:32 PM
Chronological Index c20030810 [6].pdfChronological Index c20030810 [6].pdf 872KB Mar 27 2010 11:50:32 PM
Computational study of blowing on delta wings at high alpha c20030810 [7].pdfComputational study of blowing on delta wings at high alpha c20030810 [7].pdf 873KB Mar 27 2010 11:50:32 PM
Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles c20030810 [10].pdfDesign tradeoffs on scramjet engine integrated hypersonic waverider vehicles c20030810 [10].pdf 1494KB Mar 27 2010 11:50:32 PM
Downwash measurements on a pitching canard-wing configuration c20030810 [4].pdfDownwash measurements on a pitching canard-wing configuration c20030810 [4].pdf 486KB Mar 27 2010 11:50:32 PM
Errata_ Aerospace Plane Design Challenge_ Credible Computations c20030810 [1].pdfErrata_ Aerospace Plane Design Challenge_ Credible Computations c20030810 [1].pdf 90KB Mar 27 2010 11:50:32 PM
Euler code prediction of near-field to midfield sonic boom pressure signatures c20030810 [7].pdfEuler code prediction of near-field to midfield sonic boom pressure signatures c20030810 [7].pdf 1037KB Mar 27 2010 11:50:32 PM
Experimental verification of a wall interference correction method with interface measurements c20030810 [5].pdfExperimental verification of a wall interference correction method with interface measurements c20030810 [5].pdf 557KB Mar 27 2010 11:50:32 PM
Finite element nonlinear flutter and fatigue life of two-dimensional panels with temperature effects c20030810 [8].pdfFinite element nonlinear flutter and fatigue life of two-dimensional panels with temperature effects c20030810 [8].pdf 926KB Mar 27 2010 11:50:32 PM
Forward flight trim and frequency response validation of a helicopter simulation model c20030810 [10].pdfForward flight trim and frequency response validation of a helicopter simulation model c20030810 [10].pdf 1258KB Mar 27 2010 11:50:32 PM
Fractional order calculus model of the generalized Theodorsen function c20030810 [3].pdfFractional order calculus model of the generalized Theodorsen function c20030810 [3].pdf 416KB Mar 27 2010 11:50:32 PM
Ground vortex formed by impinging jets in crossflow c20030810 [7].pdfGround vortex formed by impinging jets in crossflow c20030810 [7].pdf 895KB Mar 27 2010 11:50:32 PM
Impact of active controls technology on structural integrity c20030810 [8].pdfImpact of active controls technology on structural integrity c20030810 [8].pdf 1191KB Mar 27 2010 11:50:32 PM
In-flight source noise of an advanced large-scale single-rotation propeller c20030810 [9].pdfIn-flight source noise of an advanced large-scale single-rotation propeller c20030810 [9].pdf 1465KB Mar 27 2010 11:50:32 PM
Investigation of rotor tip vortex interactions with a body c20030810 [10].pdfInvestigation of rotor tip vortex interactions with a body c20030810 [10].pdf 1300KB Mar 27 2010 11:50:32 PM
Measurement and improvement of the lateral agility of the F-18 c20030810 [2].pdfMeasurement and improvement of the lateral agility of the F-18 c20030810 [2].pdf 268KB Mar 27 2010 11:50:32 PM
Numerical analysis of supersonic multijets c20030810 [2].pdfNumerical analysis of supersonic multijets c20030810 [2].pdf 680KB Mar 27 2010 11:50:32 PM
Numerical prediction of vortical flow over slender delta wings c20030810 [8].pdfNumerical prediction of vortical flow over slender delta wings c20030810 [8].pdf 1204KB Mar 27 2010 11:50:32 PM
Optimization of aircraft engine suspension systems c20030810 [6].pdfOptimization of aircraft engine suspension systems c20030810 [6].pdf 1010KB Mar 27 2010 11:50:32 PM
Optimization of joined-wing aircraft c20030810 [9].pdfOptimization of joined-wing aircraft c20030810 [9].pdf 1325KB Mar 27 2010 11:50:32 PM
Optimizing tuning masses for helicopter rotor blade vibration reduction and comparison with test data c20030810 [5].pdfOptimizing tuning masses for helicopter rotor blade vibration reduction and comparison with test data c20030810 [5].pdf 700KB Mar 27 2010 11:50:32 PM
Prediction of fluctuating pressure in attached and separated turbulent boundary-layer flow c20030810 [9].pdfPrediction of fluctuating pressure in attached and separated turbulent boundary-layer flow c20030810 [9].pdf 1141KB Mar 27 2010 11:50:32 PM
Response of helicopter blades to a sharp collective increase c20030810 [8].pdfResponse of helicopter blades to a sharp collective increase c20030810 [8].pdf 1052KB Mar 27 2010 11:50:32 PM
Selected design issues of some high-speed rotorcraft concepts c20030810 [8].pdfSelected design issues of some high-speed rotorcraft concepts c20030810 [8].pdf 1113KB Mar 27 2010 11:50:32 PM
Subject Index c20030810 [6].pdfSubject Index c20030810 [6].pdf 856KB Mar 27 2010 11:50:32 PM
Target pitch angle for the microburst escape maneuver c20030810 [7].pdfTarget pitch angle for the microburst escape maneuver c20030810 [7].pdf 959KB Mar 27 2010 11:50:32 PM
Thermoacoustic loads and fatigue of hypersonic vehicle skin panels c20030810 [8].pdfThermoacoustic loads and fatigue of hypersonic vehicle skin panels c20030810 [8].pdf 1229KB Mar 27 2010 11:50:32 PM
Transonic airfoil design by constrained optimization c20030810 [2].pdfTransonic airfoil design by constrained optimization c20030810 [2].pdf 215KB Mar 27 2010 11:50:32 PM
Vortex control technique for the attenuation of fin buffet c20030810 [7].pdfVortex control technique for the attenuation of fin buffet c20030810 [7].pdf 1186KB Mar 27 2010 11:50:32 PM
Vortex flow control using fillets on a double-delta wing c20030810 [8].pdfVortex flow control using fillets on a double-delta wing c20030810 [8].pdf 1164KB Mar 27 2010 11:50:32 PM